CN209917260U - Toy folding four-shaft aircraft - Google Patents
Toy folding four-shaft aircraft Download PDFInfo
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- CN209917260U CN209917260U CN201920596931.0U CN201920596931U CN209917260U CN 209917260 U CN209917260 U CN 209917260U CN 201920596931 U CN201920596931 U CN 201920596931U CN 209917260 U CN209917260 U CN 209917260U
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- 230000005540 biological transmission Effects 0.000 claims description 35
- 230000005611 electricity Effects 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 2
- 230000001174 ascending effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
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Abstract
The utility model discloses a toy folding four-shaft aircraft, which comprises a body shell, a front bracket and a camera fixing seat, wherein the front bracket is matched on the two sides of the front end of the body shell through a rotating shaft, the front end of the body shell is provided with a matching groove, the camera fixing seat is arranged in the matching groove through the matching between a circular lug and a matching hole, the aircraft also comprises a rear bracket, the two sides of the rear part of the body shell are matched with rotating blocks, the other end of the rotating block is matched in the rear bracket, the top parts of the front bracket and the rear bracket are both provided with rotating covers, the top parts of the rotating covers are provided with propellers, the bottom part of the body shell is provided with an electricity storage device, a circuit board is arranged in the body shell, a remote controller is arranged on the circuit board, and the propellers on each bracket of the aircraft are of a detachable structure, the propeller dismounting device can be dismounted when not in use, the dismounting and mounting modes of the propeller are simple and quick, and meanwhile, each support has a folding function.
Description
Technical Field
The utility model belongs to the technical field of the aircraft technique and specifically relates to a four shaft air vehicle is folded to toy.
Background
With the development of science and technology, people start to use various small aircrafts as entertainment tools, and the small aircrafts can ascend to the high altitude and capture image data through cameras arranged on the small aircrafts so as to collect pictures shot from the high altitude; however, some existing aircrafts use a single motor to drive the aircraft to ascend, so that the ascending height of the aircraft is limited, and most of cameras arranged on the aircraft are connected in a position fixing manner, so that the aircraft can capture images at certain positions only when flying to the upper space of the positions; when the aircraft is not used, the propeller and the bracket on the aircraft are relatively out of the plane relative to components on other positions, so that the possibility of external impact on the aircraft is increased, and the aircraft is easily damaged; therefore, there is a need for improvements in the construction of aircraft.
SUMMERY OF THE UTILITY MODEL
The utility model discloses not enough to above-mentioned technique provides a screw on each support for can assembling and disassembling formula structure, can demolish when not using, the screw demolish with the simple swift of mounting means, each support all has the function of folding up simultaneously, the battery is for can assembling and disassembling formula structure, the position of camera can swing the folding four shaft air vehicle of toy of adjusting.
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes:
a toy folding four-axis aircraft comprises a fuselage shell, a front support and a camera fixing seat, wherein the front support is matched on two sides of the front end of the fuselage shell through a rotating shaft, a matching groove is formed in the front end of the fuselage shell, matching holes are formed in the fuselage shell on two sides of the matching groove, circular convex blocks are arranged at two ends of the camera fixing seat, the camera fixing seat is arranged in the matching groove through the matching between the circular convex blocks and the matching holes, the aircraft further comprises a rear support, rotating blocks are matched on two sides of the rear of the fuselage shell, the other end of each rotating block is matched in the rear support, rotating covers are arranged on the tops of the front support and the rear support, propellers are arranged on the tops of the rotating covers, an electric storage device is arranged at the bottom of the fuselage shell, a circuit board is arranged in the fuselage shell, and a remote controller is arranged on the circuit board, the camera fixing seat is internally provided with a camera.
Furthermore, all be provided with first motor in fore-stock and the after-poppet, the cooperation has first drive gear on the drive end of first motor, be provided with second drive gear in the outside end of fore-stock, first drive gear is connected with second drive gear through the mode of teeth of a cogwheel meshing.
Further, the gear teeth of the second transmission gear are arranged on the surface of the second transmission gear in a ring shape.
Furthermore, the rotating cover is annularly provided with at least two rotating clamping grooves, the outer edge of the bottom of the propeller is annularly provided with at least two rotating clamping blocks, the rotating clamping blocks are matched in the rotating clamping grooves, the center of the second transmission gear is matched with a transmission rod, the transmission rod penetrates through the rotating cover and is matched with the rotating cover, and the outer side of the upper end part of the transmission rod is sleeved with a spring.
Furthermore, a steering engine is arranged on the circuit board, a connecting rod is arranged at the driving end of the steering engine, and the other end of the connecting rod is connected to the camera fixing seat.
Further, a machine door is arranged on the machine body shell outside the power storage device.
Furthermore, foot rests are arranged at the bottoms of one sides of the front support and the rear support.
The utility model has the advantages that:
the propeller on the bracket is of a detachable structure and can be detached when not in use, the detaching and installing modes of the propeller are simple and quick, and the propeller can be detached or installed by pressing down and rotating the propeller; meanwhile, the front support and the rear support have folding functions, and can be folded when not in use, so that the possibility of damage is reduced; the machine body shell is provided with a machine door which can assemble and disassemble the battery; the camera receives image data through a remote controller or performs swing adjustment on the position of the camera.
Drawings
Fig. 1 is a schematic view of the overall surface structure of the aircraft.
Fig. 2 is a schematic view of the overall bottom structure of the aircraft.
Fig. 3 is a schematic view of the overall internal structure of the aircraft.
Fig. 4 is a schematic view of the internal structure of the rear bracket.
Fig. 5 is a cross-sectional view of the propeller engaged with the rotary cap.
Fig. 6 is a schematic structural view of the propeller.
Fig. 7 is a schematic structural view of a camera fixing seat.
Fig. 8 is a schematic structural view of the rotary cap.
Fig. 9 is a schematic structural view of the aircraft in a folded state.
In the figure, a machine body shell 1, a front support 2, a camera fixing seat 3, a matching groove 4, a round bump 5, a matching hole 6, a rear support 7, a rotating block 8, a rotating cover 9, a propeller 10, an electricity storage device 11, a circuit board 12, a remote controller 13, a first motor 14, a first transmission gear 15, a second transmission gear 16, gear teeth 17, a rotating clamping groove 18, a transmission rod 19, a spring 20, a steering engine 21, a connecting rod 22, a machine door 23, a foot rest 24, a rotating shaft 25, a camera 26 and a rotating clamping block 27.
Detailed Description
As shown in fig. 1-9, the toy folding four-shaft aircraft comprises a fuselage shell 1, a front support 2 and a camera fixing seat 3, wherein the front support 2 is matched with two sides of the front end of the fuselage shell 1 through a rotating shaft 25, the front end of the fuselage shell 1 is provided with a matching groove 4, the fuselage shell 1 on two sides of the matching groove 4 is provided with a matching hole 6, two ends of the camera fixing seat 3 are provided with circular convex blocks 5, the camera fixing seat 3 is arranged in the matching groove 4 through the matching between the circular convex blocks 5 and the matching hole 6, the aircraft further comprises a rear support 7, two sides of the rear part of the fuselage shell 1 are matched with rotating blocks 8, the other end of each rotating block 8 is matched in the rear support 7, the tops of the front support 2 and the rear support 7 are both provided with rotating covers 9, the top of each rotating cover 9 is provided with a propeller 10, the bottom of fuselage casing 1 is provided with power storage device 11, be provided with circuit board 12 in the fuselage casing 1, be provided with remote control 13 on the circuit board 12, be provided with camera 26 in the camera fixing base 3.
The front support 2 and the rear support 7 are internally provided with first motors 14, the driving ends of the first motors 14 are matched with first transmission gears 15, the outer side ends of the front support 2 are internally provided with second transmission gears 16, and the first transmission gears 15 are connected with the second transmission gears 16 in a gear tooth 17 meshing mode.
The gear teeth 17 of the second transmission gear 16 are arranged on the surface of the second transmission gear 16 in a ring shape.
At least two rotary clamping grooves 18 are annularly arranged on the rotary cover 9, at least two rotary clamping blocks 27 are annularly arranged on the outer edge of the bottom of the propeller 10, the rotary clamping blocks 27 are matched in the rotary clamping grooves 18, a transmission rod 19 is matched at the center of the second transmission gear 16, the transmission rod 19 penetrates through the rotary cover 9 and is matched with the rotary cover 9, and a spring 20 is sleeved on the outer side of the upper end portion of the transmission rod 19.
The circuit board 12 is provided with a steering engine 21, a connecting rod 22 is arranged at the driving end of the steering engine 21, and the other end of the connecting rod 22 is connected to the camera fixing seat 3.
A machine door 23 is arranged on the machine body shell 1 outside the power storage device 11.
When the camera is used, the power storage device 11 is electrically connected with the camera 26, the circuit board 12, the remote controller 13, the first motor 14 and the steering engine 21 respectively, the remote controller 13 is controlled by an external remote controller to receive image data of the camera 26, the remote controller 13 can be controlled by the external remote controller to open or close the steering engine 21, the connecting rod 22 is controlled to swing by starting the steering engine 21, the camera fixing seat 3 swings up and down by swinging the connecting rod 22, and the position of the camera 26 is adjusted; the remote controller 13 is controlled by an external remote controller to start the first motor 14, the first motor 14 is started and drives the first transmission gear 15 to rotate, the first transmission gear 15 rotates and drives the second transmission gear 16 to rotate, the second transmission gear 16 rotates and drives the transmission rod 19 to rotate, the transmission rod 19 rotates and drives the rotary cover 9 to rotate, the rotary cover 9 rotates and drives the propeller 10 to rotate, and the whole aircraft flies under the driving of the propeller 10; when the folding machine is not used, the front support 2 can swing towards the direction of the machine body shell 1 by taking the rotating shaft 25 as a rotating axis, the swing amplitude of the front support 2 swings at 90 degrees on a horizontal plane, so that the front support 2 is folded at the position of the machine body shell 1, the rear support 7 can swing towards the direction of the machine body shell 1 by taking the rotating block 8 as a rotating axis, the swing amplitude of the rear support 7 swings at 180 degrees on a vertical plane, and the rear support 7 is folded at the position of the machine body shell 1; the matching between the rotating clamping block 27 and the rotating clamping groove 18 can be separated by pressing and rotating the propeller 10, and the propeller 10 is bounced up under the action of restoring the original shape through the spring 20, so that the propeller 10 is detached, when the propeller 10 is installed, the rotating clamping block 27 on the propeller 10 is aligned to the position of the rotating clamping groove 18 for installation, and then the rotating clamping block 27 is fixed in the rotating clamping groove 18 in a matching manner through rotating and pressing the propeller 10, so that the propeller 10 is installed on the rotating cover 9, when the propeller 10 is installed in the rotating cover 9, the propeller 10 can be jacked up through the spring 20, and the situation that the propeller 10 is loosened is avoided; the machine body shell 1 is provided with a machine door 23, and the operation of taking out or locking the power storage device 11 can be carried out by opening or closing the machine door 23; foot rests 24 are provided on the bottoms of the front support 2 and the rear support 7 on one side to provide a support for the aircraft on the ground.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (7)
1. A toy folding four-shaft aircraft comprises a fuselage shell, a front support and a camera fixing seat, wherein the front support is matched on two sides of the front end of the fuselage shell through a rotating shaft, a matching groove is formed in the front end of the fuselage shell, matching holes are formed in the fuselage shell on two sides of the matching groove, circular convex blocks are arranged at two ends of the camera fixing seat, the camera fixing seat is arranged in the matching groove through the matching between the circular convex blocks and the matching holes, the toy folding four-shaft aircraft is characterized by further comprising a rear support, rotating blocks are matched on two sides of the rear part of the fuselage shell, the other ends of the rotating blocks are matched in the rear support, rotating covers are arranged on the tops of the front support and the rear support, a propeller is arranged on the top of each rotating cover, an electric storage device is arranged at the bottom of the fuselage shell, a circuit board is arranged in, the circuit board is provided with a remote controller, and a camera is arranged in the camera fixing seat.
2. The toy folding quadrotor according to claim 1, wherein a first motor is arranged in each of the front support and the rear support, a first transmission gear is matched with a driving end of the first motor, a second transmission gear is arranged in an outer side end of the front support, and the first transmission gear is connected with the second transmission gear in a gear tooth meshing manner.
3. The toy folding quad bike according to claim 2, wherein the gear teeth of the second transmission gear are disposed on the surface of the second transmission gear in a ring shape.
4. The toy folding quadrotor according to claim 2, wherein the rotary cover is provided with at least two rotary clamping grooves in an annular shape, the outer edge of the bottom of the propeller is provided with at least two rotary clamping blocks in an annular shape, the rotary clamping blocks are matched in the rotary clamping grooves, the center of the second transmission gear is matched with a transmission rod, the transmission rod penetrates through the rotary cover and is matched with the rotary cover, and a spring is sleeved on the outer side of the upper end portion of the transmission rod.
5. The toy folding four-axis aircraft according to claim 1, wherein the circuit board is provided with a steering engine, a driving end of the steering engine is provided with a connecting rod, and the other end of the connecting rod is connected to the camera fixing seat.
6. The toy folding quadcopter of claim 1, wherein a door is provided on the fuselage housing outside the electrical storage device.
7. The toy folding quadcopter of claim 1, wherein a foot rest is provided at the bottom of one side of the front and rear supports.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920596931.0U CN209917260U (en) | 2019-04-28 | 2019-04-28 | Toy folding four-shaft aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920596931.0U CN209917260U (en) | 2019-04-28 | 2019-04-28 | Toy folding four-shaft aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209917260U true CN209917260U (en) | 2020-01-10 |
Family
ID=69089730
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920596931.0U Expired - Fee Related CN209917260U (en) | 2019-04-28 | 2019-04-28 | Toy folding four-shaft aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209917260U (en) |
-
2019
- 2019-04-28 CN CN201920596931.0U patent/CN209917260U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200110 |